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 48222U 26145.63702668 +.00000000 +00000-0 +81858-3 0 00000
2 48222 87.8934 294.2024 0001717 98.5727 261.5597 13.14503633 00
| Epoch (UTC): | 25 May 2026 15:17:19 |
| Eccentricity: | 0.0001717 |
| inclination: | 87.8934° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2024° |
| argument of perigee: | 98.5727° |
| revolutions per day: | 13.14503633 |
| mean anomaly at epoch: | 261.5597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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