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 26069.93915365 +.00000000 +00000-0 +38097-3 0 00009
2 28895 98.2837 223.5865 0014810 153.7429 206.4532 14.72326757 03
| Epoch (UTC): | 10 March 2026 22:32:22 |
| Eccentricity: | 0.0014810 |
| inclination: | 98.2837° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 223.5865° |
| argument of perigee: | 153.7429° |
| revolutions per day: | 14.72326757 |
| mean anomaly at epoch: | 206.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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