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 53288U 26145.43494558 +.00000000 +00000-0 +15663-4 0 00004
2 53288 53.2118 199.5991 0001314 84.8028 275.3114 15.08840818 06
| Epoch (UTC): | 25 May 2026 10:26:19 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.5991° |
| argument of perigee: | 84.8028° |
| revolutions per day: | 15.08840818 |
| mean anomaly at epoch: | 275.3114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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