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 23030.58246321 .00004036 00000-0 51562-3 0 9993
2 00107 28.7889 170.5324 0537600 222.7579 132.9947 14.11235834101390
| Epoch (UTC): | 30 January 2023 13:58:44 |
| Eccentricity: | 0.0537600 |
| inclination: | 28.7889° |
| perigee height: | 466 km |
| apogee height: | 1244 km |
| right ascension of ascending node: | 170.5324° |
| argument of perigee: | 222.7579° |
| revolutions per day: | 14.11235834 |
| mean anomaly at epoch: | 132.9947° |
| orbit number at epoch: | 10139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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