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 52497U 26145.05912580 +.00000000 +00000-0 -12783-4 0 00004
2 52497 53.2144 66.2821 0001266 89.4964 270.6174 15.08839554 03
| Epoch (UTC): | 25 May 2026 01:25:08 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 66.2821° |
| argument of perigee: | 89.4964° |
| revolutions per day: | 15.08839554 |
| mean anomaly at epoch: | 270.6174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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