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 48793U 26145.30952498 +.00000000 +00000-0 +39077-3 0 00001
2 48793 87.8994 263.7510 0001777 91.8860 268.2474 13.15548508 09
| Epoch (UTC): | 25 May 2026 07:25:42 |
| Eccentricity: | 0.0001777 |
| inclination: | 87.8994° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7510° |
| argument of perigee: | 91.8860° |
| revolutions per day: | 13.15548508 |
| mean anomaly at epoch: | 268.2474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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