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 25868U 99040C 25131.81229766 .00012514 00000-0 78542-3 0 9996
2 25868 28.4944 312.4546 4396107 300.5887 23.2963 6.72620895586355
| Epoch (UTC): | 11 May 2025 19:29:42 |
| Eccentricity: | 0.4396107 |
| inclination: | 28.4944° |
| perigee height: | 265 km |
| apogee height: | 10688 km |
| right ascension of ascending node: | 312.4546° |
| argument of perigee: | 300.5887° |
| revolutions per day: | 6.72620895 |
| mean anomaly at epoch: | 23.2963° |
| orbit number at epoch: | 58635 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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