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 48229U 26145.66238153 +.00000000 +00000-0 -45432-3 0 00002
2 48229 87.8950 294.1869 0001818 101.6083 258.5251 13.14501215 01
| Epoch (UTC): | 25 May 2026 15:53:49 |
| Eccentricity: | 0.0001818 |
| inclination: | 87.8950° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.1869° |
| argument of perigee: | 101.6083° |
| revolutions per day: | 13.14501215 |
| mean anomaly at epoch: | 258.5251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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