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 48071U 26145.22085910 +.00000000 +00000-0 -80792-3 0 00008
2 48071 87.8947 324.7946 0001614 92.7264 267.4050 13.13469659 03
| Epoch (UTC): | 25 May 2026 05:18:02 |
| Eccentricity: | 0.0001614 |
| inclination: | 87.8947° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7946° |
| argument of perigee: | 92.7264° |
| revolutions per day: | 13.13469659 |
| mean anomaly at epoch: | 267.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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