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 is defined by the following mean orbital elements,
1 53807U 26039.08257134 +.00000000 +00000-0 +18024-3 0 00004
2 53807 53.2286 279.3818 0007951 128.0822 232.0901 15.36706816 04
| Epoch (UTC): | 08 February 2026 01:58:54 |
| Eccentricity: | 0.0007951 |
| inclination: | 53.2286° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 279.3818° |
| argument of perigee: | 128.0822° |
| revolutions per day: | 15.36706816 |
| mean anomaly at epoch: | 232.0901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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