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 48963U 26145.34480859 +.00000000 +00000-0 +64534-3 0 00007
2 48963 97.6775 341.4350 0000552 112.6705 247.4624 15.88406855 06
| Epoch (UTC): | 25 May 2026 08:16:31 |
| Eccentricity: | 0.0000552 |
| inclination: | 97.6775° |
| perigee height: | 306 km |
| apogee height: | 307 km |
| right ascension of ascending node: | 341.4350° |
| argument of perigee: | 112.6705° |
| revolutions per day: | 15.88406855 |
| mean anomaly at epoch: | 247.4624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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