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 42214U 81053UE 23323.70553610 .00001612 00000-0 15362-2 0 9999
2 42214 83.0188 110.6837 0092517 265.6977 93.3605 13.78245290825692
| Epoch (UTC): | 19 November 2023 16:55:58 |
| Eccentricity: | 0.0092517 |
| inclination: | 83.0188° |
| perigee height: | 902 km |
| apogee height: | 1038 km |
| right ascension of ascending node: | 110.6837° |
| argument of perigee: | 265.6977° |
| revolutions per day: | 13.78245290 |
| mean anomaly at epoch: | 93.3605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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