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 25481U 26145.27905353 +.00000000 +00000-0 +31589-3 0 00004
2 25481 45.0051 84.1536 0001350 322.9684 37.1071 14.39088109 09
| Epoch (UTC): | 25 May 2026 06:41:50 |
| Eccentricity: | 0.0001350 |
| inclination: | 45.0051° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 84.1536° |
| argument of perigee: | 322.9684° |
| revolutions per day: | 14.39088109 |
| mean anomaly at epoch: | 37.1071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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