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 48234U 26145.42611097 +.00000000 +00000-0 -20413-4 0 00007
2 48234 87.8951 294.2342 0001932 92.6644 267.4707 13.14502103 06
| Epoch (UTC): | 25 May 2026 10:13:35 |
| Eccentricity: | 0.0001932 |
| inclination: | 87.8951° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2342° |
| argument of perigee: | 92.6644° |
| revolutions per day: | 13.14502103 |
| mean anomaly at epoch: | 267.4707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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