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 26087.55006449 +.00000000 +00000-0 +15152-3 0 00005
2 27848 98.6807 96.8929 0010614 79.7322 280.5053 14.23574119 04
| Epoch (UTC): | 28 March 2026 13:12:05 |
| Eccentricity: | 0.0010614 |
| inclination: | 98.6807° |
| perigee height: | 806 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 96.8929° |
| argument of perigee: | 79.7322° |
| revolutions per day: | 14.23574119 |
| mean anomaly at epoch: | 280.5053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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