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 21023.43002471 .00001420 00000-0 57472-4 0 9993
2 42015 97.3320 92.1083 0004604 262.7538 97.3177 15.26305837218890
| Epoch (UTC): | 23 January 2021 10:19:14 |
| Eccentricity: | 0.0004604 |
| inclination: | 97.3320° |
| perigee height: | 484 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 92.1083° |
| argument of perigee: | 262.7538° |
| revolutions per day: | 15.26305837 |
| mean anomaly at epoch: | 97.3177° |
| orbit number at epoch: | 21889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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