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 21088U 91006B 23266.13180663 .00000157 00000-0 14259-3 0 9999
2 21088 82.9396 118.4233 0023358 34.4764 87.7266 13.77270836640649
| Epoch (UTC): | 23 September 2023 03:09:48 |
| Eccentricity: | 0.0023358 |
| inclination: | 82.9396° |
| perigee height: | 956 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 118.4233° |
| argument of perigee: | 34.4764° |
| revolutions per day: | 13.77270836 |
| mean anomaly at epoch: | 87.7266° |
| orbit number at epoch: | 64064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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