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 48065U 26145.21747536 +.00000000 +00000-0 -67404-3 0 00004
2 48065 87.8951 324.7761 0001889 97.1057 263.0287 13.13470551 06
| Epoch (UTC): | 25 May 2026 05:13:09 |
| Eccentricity: | 0.0001889 |
| inclination: | 87.8951° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7761° |
| argument of perigee: | 97.1057° |
| revolutions per day: | 13.13470551 |
| mean anomaly at epoch: | 263.0287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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