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 26106.70384451 +.00000000 +00000-0 +14455-3 0 00004
2 28895 98.2906 261.0661 0014850 44.9479 315.2927 14.72467493 01
| Epoch (UTC): | 16 April 2026 16:53:32 |
| Eccentricity: | 0.0014850 |
| inclination: | 98.2906° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 261.0661° |
| argument of perigee: | 44.9479° |
| revolutions per day: | 14.72467493 |
| mean anomaly at epoch: | 315.2927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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