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 25989U 26135.43881895 +.00000000 +00000-0 +00000-0 0 00009
2 25989 64.6604 283.4024 4685414 65.5061 0.1256 0.50124669 06
| Epoch (UTC): | 15 May 2026 10:31:53 |
| Eccentricity: | 0.4685414 |
| inclination: | 64.6604° |
| perigee height: | 29199 km |
| apogee height: | 91929 km |
| right ascension of ascending node: | 283.4024° |
| argument of perigee: | 65.5061° |
| revolutions per day: | 0.50124669 |
| mean anomaly at epoch: | 0.1256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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