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 48219U 26145.43245558 +.00000000 +00000-0 -36704-3 0 00005
2 48219 87.8942 294.2430 0002020 99.6684 260.4674 13.14501770 02
| Epoch (UTC): | 25 May 2026 10:22:44 |
| Eccentricity: | 0.0002020 |
| inclination: | 87.8942° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2430° |
| argument of perigee: | 99.6684° |
| revolutions per day: | 13.14501770 |
| mean anomaly at epoch: | 260.4674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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