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 48976U 26145.53324245 +.00000000 +00000-0 +28131-3 0 00001
2 48976 87.9107 233.2805 0001958 101.7956 258.3394 13.16593174 07
| Epoch (UTC): | 25 May 2026 12:47:52 |
| Eccentricity: | 0.0001958 |
| inclination: | 87.9107° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2805° |
| argument of perigee: | 101.7956° |
| revolutions per day: | 13.16593174 |
| mean anomaly at epoch: | 258.3394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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