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 28895U 26038.94758153 +.00000000 +00000-0 +38429-3 0 00005
2 28895 98.2780 192.0225 0013248 254.3792 105.5953 14.72183585 01
| Epoch (UTC): | 07 February 2026 22:44:31 |
| Eccentricity: | 0.0013248 |
| inclination: | 98.2780° |
| perigee height: | 645 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 192.0225° |
| argument of perigee: | 254.3792° |
| revolutions per day: | 14.72183585 |
| mean anomaly at epoch: | 105.5953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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