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 18025U 26076.28780411 +.00000000 +00000-0 +63325-3 0 00003
2 18025 63.2877 251.5453 0789409 101.6423 267.4235 13.88780865 03
| Epoch (UTC): | 17 March 2026 06:54:26 |
| Eccentricity: | 0.0789409 |
| inclination: | 63.2877° |
| perigee height: | 356 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 251.5453° |
| argument of perigee: | 101.6423° |
| revolutions per day: | 13.88780865 |
| mean anomaly at epoch: | 267.4235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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