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 48781U 26145.55671015 +.00000000 +00000-0 +34977-3 0 00002
2 48781 87.9007 263.6910 0001844 102.1697 257.9640 13.15549362 03
| Epoch (UTC): | 25 May 2026 13:21:39 |
| Eccentricity: | 0.0001844 |
| inclination: | 87.9007° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6910° |
| argument of perigee: | 102.1697° |
| revolutions per day: | 13.15549362 |
| mean anomaly at epoch: | 257.9640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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