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 48280U 26145.13620532 +.00000000 +00000-0 +79009-4 0 00004
2 48280 53.1594 105.6309 0001280 67.1903 292.9233 15.31690874 06
| Epoch (UTC): | 25 May 2026 03:16:08 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 105.6309° |
| argument of perigee: | 67.1903° |
| revolutions per day: | 15.31690874 |
| mean anomaly at epoch: | 292.9233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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