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 52935U 26145.41105567 +.00000000 +00000-0 +22421-3 0 00008
2 52935 9.9945 354.1624 0004164 335.6280 24.3739 15.13647729 02
| Epoch (UTC): | 25 May 2026 09:51:55 |
| Eccentricity: | 0.0004164 |
| inclination: | 9.9945° |
| perigee height: | 522 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 354.1624° |
| argument of perigee: | 335.6280° |
| revolutions per day: | 15.13647729 |
| mean anomaly at epoch: | 24.3739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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