View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 40299U 14070B 25071.95297130 .09800336 23785-5 25667-3 0 9995
2 40299 97.0580 141.6997 0009515 258.4705 101.5529 16.45130457577203
| Epoch (UTC): | 12 March 2025 22:52:16 |
| Eccentricity: | 0.0009515 |
| inclination: | 97.0580° |
| perigee height: | 146 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 141.6997° |
| argument of perigee: | 258.4705° |
| revolutions per day: | 16.45130457 |
| mean anomaly at epoch: | 101.5529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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