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3 changes: 2 additions & 1 deletion docs/source/quickstart.md
Original file line number Diff line number Diff line change
Expand Up @@ -157,6 +157,7 @@ The `propagate` method gives you the final orbit at the epoch you designated. To
```python
from hapsira.twobody.sampling import EpochsArray, TrueAnomalyBounds, EpochBounds
from hapsira.util import time_range
from astropy.time import Time

start_date = Time("2022-07-11 05:05", scale="utc")
end_date = Time("2022-07-11 07:05", scale="utc")
Expand All @@ -165,7 +166,7 @@ end_date = Time("2022-07-11 07:05", scale="utc")
ephem1 = iss.to_ephem()

# Explicit times given
ephem2 = iss.to_ephem(strategy=EpochsArray(epochs=time_range(start_date, end_date)))
ephem2 = iss.to_ephem(strategy=EpochsArray(epochs=time_range(start=start_date, end=end_date)))

# Automatic grid, true anomaly limits
ephem3 = iss.to_ephem(strategy=TrueAnomalyBounds(min_nu=0 << u.deg, max_nu=180 << u.deg))
Expand Down