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 52630U 26145.36273403 +.00000000 +00000-0 -60816-4 0 00001
2 52630 53.2136 284.9209 0001501 96.6988 263.4175 15.08840157 02
| Epoch (UTC): | 25 May 2026 08:42:20 |
| Eccentricity: | 0.0001501 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.9209° |
| argument of perigee: | 96.6988° |
| revolutions per day: | 15.08840157 |
| mean anomaly at epoch: | 263.4175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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