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 48244U 26145.36425216 +.00000000 +00000-0 -48295-3 0 00004
2 48244 87.8941 294.2428 0001772 101.4758 258.6571 13.14501262 04
| Epoch (UTC): | 25 May 2026 08:44:31 |
| Eccentricity: | 0.0001772 |
| inclination: | 87.8941° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2428° |
| argument of perigee: | 101.4758° |
| revolutions per day: | 13.14501262 |
| mean anomaly at epoch: | 258.6571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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