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 10121U 77059B 23333.88828498 .00000560 00000-0 19940-3 0 9999
2 10121 74.0453 128.2158 0019816 259.2460 100.6462 14.36459412428147
| Epoch (UTC): | 29 November 2023 21:19:07 |
| Eccentricity: | 0.0019816 |
| inclination: | 74.0453° |
| perigee height: | 756 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 128.2158° |
| argument of perigee: | 259.2460° |
| revolutions per day: | 14.36459412 |
| mean anomaly at epoch: | 100.6462° |
| orbit number at epoch: | 42814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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