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 26031.72532400 +.00000000 +00000-0 +00000-0 0 00001
2 25989 65.1743 284.7836 4724780 67.3227 359.9893 0.50131279 02
| Epoch (UTC): | 31 January 2026 17:24:27 |
| Eccentricity: | 0.4724780 |
| inclination: | 65.1743° |
| perigee height: | 28932 km |
| apogee height: | 92184 km |
| right ascension of ascending node: | 284.7836° |
| argument of perigee: | 67.3227° |
| revolutions per day: | 0.50131279 |
| mean anomaly at epoch: | 359.9893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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