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 26105.84809374 +.00000000 +00000-0 +53985-4 0 00002
2 28891 98.2980 243.4474 0016939 117.6338 242.6587 14.64485267 02
| Epoch (UTC): | 15 April 2026 20:21:15 |
| Eccentricity: | 0.0016939 |
| inclination: | 98.2980° |
| perigee height: | 667 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 243.4474° |
| argument of perigee: | 117.6338° |
| revolutions per day: | 14.64485267 |
| mean anomaly at epoch: | 242.6587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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