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 data is extracted from the following two-line orbital elements,
1 42015U 17008BV 23088.73262073 .00052598 00000-0 11270-2 0 9991
2 42015 97.2189 152.3273 0002511 299.8286 60.2713 15.44589731340560
| Epoch (UTC): | 29 March 2023 17:34:58 |
| Eccentricity: | 0.0002511 |
| inclination: | 97.2189° |
| perigee height: | 431 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 152.3273° |
| argument of perigee: | 299.8286° |
| revolutions per day: | 15.44589731 |
| mean anomaly at epoch: | 60.2713° |
| orbit number at epoch: | 34056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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