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 26145.36827770 +.00000000 +00000-0 +19515-3 0 00007
2 28895 98.2961 300.5153 0012780 278.4660 81.5098 14.72559828 09
| Epoch (UTC): | 25 May 2026 08:50:19 |
| Eccentricity: | 0.0012780 |
| inclination: | 98.2961° |
| perigee height: | 644 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 300.5153° |
| argument of perigee: | 278.4660° |
| revolutions per day: | 14.72559828 |
| mean anomaly at epoch: | 81.5098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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