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 24255.55357345 .00005766 00000-0 71548-3 0 9996
2 00107 28.7911 54.1519 0516111 258.9437 95.2692 14.16609882184940
| Epoch (UTC): | 11 September 2024 13:17:08 |
| Eccentricity: | 0.0516111 |
| inclination: | 28.7911° |
| perigee height: | 464 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 54.1519° |
| argument of perigee: | 258.9437° |
| revolutions per day: | 14.16609882 |
| mean anomaly at epoch: | 95.2692° |
| orbit number at epoch: | 18494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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