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 48223U 26145.38805382 +.00000000 +00000-0 +34537-3 0 00002
2 48223 87.8939 294.2437 0001866 106.3322 253.8013 13.14503338 07
| Epoch (UTC): | 25 May 2026 09:18:47 |
| Eccentricity: | 0.0001866 |
| inclination: | 87.8939° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2437° |
| argument of perigee: | 106.3322° |
| revolutions per day: | 13.14503338 |
| mean anomaly at epoch: | 253.8013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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