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 52494U 26145.18424060 +.00000000 +00000-0 -60250-4 0 00008
2 52494 53.2141 65.7199 0001217 80.4584 279.6546 15.08844032 03
| Epoch (UTC): | 25 May 2026 04:25:18 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 65.7199° |
| argument of perigee: | 80.4584° |
| revolutions per day: | 15.08844032 |
| mean anomaly at epoch: | 279.6546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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