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 48274U 26065.83578792 +.00000000 +00000-0 +30829-3 0 00001
2 48274 41.4663 225.5243 0006950 255.9346 104.0720 15.60495557 09
| Epoch (UTC): | 06 March 2026 20:03:32 |
| Eccentricity: | 0.0006950 |
| inclination: | 41.4663° |
| perigee height: | 382 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 225.5243° |
| argument of perigee: | 255.9346° |
| revolutions per day: | 15.60495557 |
| mean anomaly at epoch: | 104.0720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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