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 28891U 26053.64733072 +.00000000 +00000-0 +11270-3 0 00003
2 28891 98.2877 190.8637 0014604 283.7164 76.2412 14.64414427 00
| Epoch (UTC): | 22 February 2026 15:32:09 |
| Eccentricity: | 0.0014604 |
| inclination: | 98.2877° |
| perigee height: | 669 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 190.8637° |
| argument of perigee: | 283.7164° |
| revolutions per day: | 14.64414427 |
| mean anomaly at epoch: | 76.2412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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