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 00107U 61013A 23037.65521611 .00004603 00000-0 59151-3 0 9998
2 00107 28.7912 130.4467 0537416 287.6785 66.5831 14.11298104102398
| Epoch (UTC): | 06 February 2023 15:43:30 |
| Eccentricity: | 0.0537416 |
| inclination: | 28.7912° |
| perigee height: | 466 km |
| apogee height: | 1243 km |
| right ascension of ascending node: | 130.4467° |
| argument of perigee: | 287.6785° |
| revolutions per day: | 14.11298104 |
| mean anomaly at epoch: | 66.5831° |
| orbit number at epoch: | 10239 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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