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 26073.28714127 +.00000000 +00000-0 +14464-3 0 00008
2 53807 53.2290 119.1256 0004560 242.5842 117.4699 15.37206460 04
| Epoch (UTC): | 14 March 2026 06:53:29 |
| Eccentricity: | 0.0004560 |
| inclination: | 53.2290° |
| perigee height: | 451 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 119.1256° |
| argument of perigee: | 242.5842° |
| revolutions per day: | 15.37206460 |
| mean anomaly at epoch: | 117.4699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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