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 26019.24393032 +.00000000 +00000-0 +21811-3 0 00006
2 53807 53.2314 12.2702 0008353 76.8672 283.3264 15.36343480 07
| Epoch (UTC): | 19 January 2026 05:51:15 |
| Eccentricity: | 0.0008353 |
| inclination: | 53.2314° |
| perigee height: | 451 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 12.2702° |
| argument of perigee: | 76.8672° |
| revolutions per day: | 15.36343480 |
| mean anomaly at epoch: | 283.3264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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