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 61525U 26145.28091637 +.00000000 +00000-0 +69034-4 0 00002
2 61525 53.1597 146.3397 0001247 85.1276 274.9867 15.30207992 08
| Epoch (UTC): | 25 May 2026 06:44:31 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.3397° |
| argument of perigee: | 85.1276° |
| revolutions per day: | 15.30207992 |
| mean anomaly at epoch: | 274.9867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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