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 26158.19028350 +.00000000 +00000-0 +55659-3 0 00008
2 25979 98.1605 249.5164 0004887 132.0380 228.1277 15.34574610 03
| Epoch (UTC): | 07 June 2026 04:34:00 |
| Eccentricity: | 0.0004887 |
| inclination: | 98.1605° |
| perigee height: | 459 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 249.5164° |
| argument of perigee: | 132.0380° |
| revolutions per day: | 15.34574610 |
| mean anomaly at epoch: | 228.1277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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