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 26107.51489080 +.00000000 +00000-0 +00000-0 0 00007
2 25989 64.7975 283.7611 4695688 66.0082 0.0027 0.50125090 00
| Epoch (UTC): | 17 April 2026 12:21:26 |
| Eccentricity: | 0.4695688 |
| inclination: | 64.7975° |
| perigee height: | 29130 km |
| apogee height: | 91998 km |
| right ascension of ascending node: | 283.7611° |
| argument of perigee: | 66.0082° |
| revolutions per day: | 0.50125090 |
| mean anomaly at epoch: | 0.0027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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