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 48220U 26145.38248784 +.00000000 +00000-0 -42970-3 0 00007
2 48220 87.8953 294.2449 0002033 108.8014 251.3336 13.14503193 05
| Epoch (UTC): | 25 May 2026 09:10:46 |
| Eccentricity: | 0.0002033 |
| inclination: | 87.8953° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2449° |
| argument of perigee: | 108.8014° |
| revolutions per day: | 13.14503193 |
| mean anomaly at epoch: | 251.3336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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