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 36794U 10034C 23154.40596044 .00003433 00000-0 99988-3 0 9993
2 36794 49.4824 286.8100 5478337 178.4828 184.5179 4.81473137221482
| Epoch (UTC): | 03 June 2023 09:44:34 |
| Eccentricity: | 0.5478337 |
| inclination: | 49.4824° |
| perigee height: | 320 km |
| apogee height: | 16552 km |
| right ascension of ascending node: | 286.8100° |
| argument of perigee: | 178.4828° |
| revolutions per day: | 4.81473137 |
| mean anomaly at epoch: | 184.5179° |
| orbit number at epoch: | 22148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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