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 52489U 26145.52557088 +.00000000 +00000-0 +20870-3 0 00009
2 52489 53.2129 74.1894 0001090 85.3352 274.7764 15.08834615 09
| Epoch (UTC): | 25 May 2026 12:36:49 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.1894° |
| argument of perigee: | 85.3352° |
| revolutions per day: | 15.08834615 |
| mean anomaly at epoch: | 274.7764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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