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 48979U 26145.48812699 +.00000000 +00000-0 +11077-3 0 00004
2 48979 87.9103 233.2912 0001798 92.2362 267.8975 13.16594226 01
| Epoch (UTC): | 25 May 2026 11:42:54 |
| Eccentricity: | 0.0001798 |
| inclination: | 87.9103° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2912° |
| argument of perigee: | 92.2362° |
| revolutions per day: | 13.16594226 |
| mean anomaly at epoch: | 267.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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