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 27848U 26152.00092912 +.00000000 +00000-0 +14576-3 0 00007
2 27848 98.6768 160.4891 0008289 248.3946 111.6350 14.23611465 07
| Epoch (UTC): | 01 June 2026 00:01:20 |
| Eccentricity: | 0.0008289 |
| inclination: | 98.6768° |
| perigee height: | 807 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 160.4891° |
| argument of perigee: | 248.3946° |
| revolutions per day: | 14.23611465 |
| mean anomaly at epoch: | 111.6350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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