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 25137.87894665 .00006325 00000-0 77042-3 0 9999
2 00107 28.7860 71.3169 0504736 43.4643 320.4607 14.19602495220228
| Epoch (UTC): | 17 May 2025 21:05:40 |
| Eccentricity: | 0.0504736 |
| inclination: | 28.7860° |
| perigee height: | 463 km |
| apogee height: | 1190 km |
| right ascension of ascending node: | 71.3169° |
| argument of perigee: | 43.4643° |
| revolutions per day: | 14.19602495 |
| mean anomaly at epoch: | 320.4607° |
| orbit number at epoch: | 22022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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