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 26153.38988296 +.00000000 +00000-0 +00000-0 0 00006
2 25989 64.5660 283.1750 4678287 65.1499 0.1702 0.50127783 07
| Epoch (UTC): | 02 June 2026 09:21:25 |
| Eccentricity: | 0.4678287 |
| inclination: | 64.5660° |
| perigee height: | 29245 km |
| apogee height: | 91878 km |
| right ascension of ascending node: | 283.1750° |
| argument of perigee: | 65.1499° |
| revolutions per day: | 0.50127783 |
| mean anomaly at epoch: | 0.1702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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