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 25489U 26140.33627792 +.00000000 +00000-0 +67591-4 0 00005
2 25489 84.9832 351.7253 0009957 144.3830 215.8040 14.51823123 03
| Epoch (UTC): | 20 May 2026 08:04:14 |
| Eccentricity: | 0.0009957 |
| inclination: | 84.9832° |
| perigee height: | 713 km |
| apogee height: | 727 km |
| right ascension of ascending node: | 351.7253° |
| argument of perigee: | 144.3830° |
| revolutions per day: | 14.51823123 |
| mean anomaly at epoch: | 215.8040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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