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 30288U 99025YZ 23335.28440024 .00007481 00000-0 33743-2 0 9998
2 30288 99.4387 349.0560 0025216 285.1068 140.1234 14.22303725869766
| Epoch (UTC): | 01 December 2023 06:49:32 |
| Eccentricity: | 0.0025216 |
| inclination: | 99.4387° |
| perigee height: | 799 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 349.0560° |
| argument of perigee: | 285.1068° |
| revolutions per day: | 14.22303725 |
| mean anomaly at epoch: | 140.1234° |
| orbit number at epoch: | 86976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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