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 08846U 26139.66392536 +.00000000 +00000-0 +80122-5 0 00008
2 08846 81.2267 20.2592 0038956 174.4870 185.6738 14.09017118 06
| Epoch (UTC): | 19 May 2026 15:56:03 |
| Eccentricity: | 0.0038956 |
| inclination: | 81.2267° |
| perigee height: | 835 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 20.2592° |
| argument of perigee: | 174.4870° |
| revolutions per day: | 14.09017118 |
| mean anomaly at epoch: | 185.6738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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