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 27844U 26069.96884095 +.00000000 +00000-0 +19968-3 0 00006
2 27844 98.6779 79.7517 0010704 109.1603 251.0735 14.24267366 05
| Epoch (UTC): | 10 March 2026 23:15:07 |
| Eccentricity: | 0.0010704 |
| inclination: | 98.6779° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 79.7517° |
| argument of perigee: | 109.1603° |
| revolutions per day: | 14.24267366 |
| mean anomaly at epoch: | 251.0735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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