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 52642U 26145.37836748 +.00000000 +00000-0 +27793-4 0 00008
2 52642 53.2152 274.8508 0001147 93.1141 266.9982 15.08835914 01
| Epoch (UTC): | 25 May 2026 09:04:50 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.8508° |
| argument of perigee: | 93.1141° |
| revolutions per day: | 15.08835914 |
| mean anomaly at epoch: | 266.9982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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