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 25979U 26116.50303711 +.00000000 +00000-0 +66700-3 0 00003
2 25979 98.1594 203.4846 0002898 268.1448 91.9460 15.33131009 02
| Epoch (UTC): | 26 April 2026 12:04:22 |
| Eccentricity: | 0.0002898 |
| inclination: | 98.1594° |
| perigee height: | 464 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 203.4846° |
| argument of perigee: | 268.1448° |
| revolutions per day: | 15.33131009 |
| mean anomaly at epoch: | 91.9460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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