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 23087.72519884 .00002553 00000-0 32102-3 0 9999
2 00107 28.7858 206.5314 0535920 27.5565 335.2387 14.11684155109471
| Epoch (UTC): | 28 March 2023 17:24:17 |
| Eccentricity: | 0.0535920 |
| inclination: | 28.7858° |
| perigee height: | 466 km |
| apogee height: | 1241 km |
| right ascension of ascending node: | 206.5314° |
| argument of perigee: | 27.5565° |
| revolutions per day: | 14.11684155 |
| mean anomaly at epoch: | 335.2387° |
| orbit number at epoch: | 10947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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