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 26040.37488551 +.00000000 +00000-0 +37500-3 0 00006
2 28895 98.2782 193.4756 0013277 249.5584 110.4197 14.72190530 07
| Epoch (UTC): | 09 February 2026 08:59:50 |
| Eccentricity: | 0.0013277 |
| inclination: | 98.2782° |
| perigee height: | 645 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 193.4756° |
| argument of perigee: | 249.5584° |
| revolutions per day: | 14.72190530 |
| mean anomaly at epoch: | 110.4197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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