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 26106.66798200 +.00000000 +00000-0 +58407-4 0 00002
2 28891 98.2982 244.2739 0016969 115.2168 245.0795 14.64485855 06
| Epoch (UTC): | 16 April 2026 16:01:53 |
| Eccentricity: | 0.0016969 |
| inclination: | 98.2982° |
| perigee height: | 667 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 244.2739° |
| argument of perigee: | 115.2168° |
| revolutions per day: | 14.64485855 |
| mean anomaly at epoch: | 245.0795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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