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 53252U 26145.41194272 +.00000000 +00000-0 +36653-4 0 00005
2 53252 53.2108 209.6527 0001192 83.3004 276.8124 15.08836400 05
| Epoch (UTC): | 25 May 2026 09:53:11 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.6527° |
| argument of perigee: | 83.3004° |
| revolutions per day: | 15.08836400 |
| mean anomaly at epoch: | 276.8124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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