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 48794U 26145.57729904 +.00000000 +00000-0 -29750-4 0 00004
2 48794 87.8993 263.7325 0001420 126.5940 233.5321 13.15549738 05
| Epoch (UTC): | 25 May 2026 13:51:18 |
| Eccentricity: | 0.0001420 |
| inclination: | 87.8993° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7325° |
| argument of perigee: | 126.5940° |
| revolutions per day: | 13.15549738 |
| mean anomaly at epoch: | 233.5321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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