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 52477U 26145.50074211 +.00000000 +00000-0 +56767-3 0 00000
2 52477 53.2125 64.3009 0001238 97.2815 262.8318 15.08793717 01
| Epoch (UTC): | 25 May 2026 12:01:04 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.3009° |
| argument of perigee: | 97.2815° |
| revolutions per day: | 15.08793717 |
| mean anomaly at epoch: | 262.8318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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