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 26100.18025218 +.00000000 +00000-0 +26375-3 0 00007
2 28895 98.2895 254.4130 0015144 64.3466 295.9303 14.72455492 02
| Epoch (UTC): | 10 April 2026 04:19:33 |
| Eccentricity: | 0.0015144 |
| inclination: | 98.2895° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 254.4130° |
| argument of perigee: | 64.3466° |
| revolutions per day: | 14.72455492 |
| mean anomaly at epoch: | 295.9303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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