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 52880U 26145.09362684 +.00000000 +00000-0 -97205-5 0 00001
2 52880 53.2129 31.1311 0001197 76.3014 283.8111 15.08836983 01
| Epoch (UTC): | 25 May 2026 02:14:49 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.1311° |
| argument of perigee: | 76.3014° |
| revolutions per day: | 15.08836983 |
| mean anomaly at epoch: | 283.8111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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