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 22284U 92093A 23342.36391893 -.00000233 00000-0 -98430-4 0 9995
2 22284 70.9788 316.7718 0019753 205.6101 154.4044 14.13486669596552
| Epoch (UTC): | 08 December 2023 08:44:02 |
| Eccentricity: | 0.0019753 |
| inclination: | 70.9788° |
| perigee height: | 833 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 316.7718° |
| argument of perigee: | 205.6101° |
| revolutions per day: | 14.13486669 |
| mean anomaly at epoch: | 154.4044° |
| orbit number at epoch: | 59655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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