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 52904U 26145.38795063 +.00000000 +00000-0 +00000-0 0 00002
2 52904 0.0350 17.7277 0001891 354.8437 101.5651 1.00271002 06
| Epoch (UTC): | 25 May 2026 09:18:38 |
| Eccentricity: | 0.0001891 |
| inclination: | 0.0350° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 17.7277° |
| argument of perigee: | 354.8437° |
| revolutions per day: | 1.00271002 |
| mean anomaly at epoch: | 101.5651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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