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 52453U 26145.54306598 +.00000000 +00000-0 -12632-3 0 00008
2 52453 53.2144 84.1059 0001380 82.2188 277.8961 15.08834612 06
| Epoch (UTC): | 25 May 2026 13:02:00 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1059° |
| argument of perigee: | 82.2188° |
| revolutions per day: | 15.08834612 |
| mean anomaly at epoch: | 277.8961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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