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 26044.38489903 +.00000000 +00000-0 +34420-3 0 00001
2 28895 98.2782 197.5584 0013388 235.8477 124.1461 14.72207793 09
| Epoch (UTC): | 13 February 2026 09:14:15 |
| Eccentricity: | 0.0013388 |
| inclination: | 98.2782° |
| perigee height: | 645 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 197.5584° |
| argument of perigee: | 235.8477° |
| revolutions per day: | 14.72207793 |
| mean anomaly at epoch: | 124.1461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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