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 26071.97796088 +.00000000 +00000-0 +37351-3 0 00007
2 28895 98.2837 225.6641 0014896 147.5945 212.6180 14.72336828 04
| Epoch (UTC): | 12 March 2026 23:28:15 |
| Eccentricity: | 0.0014896 |
| inclination: | 98.2837° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 225.6641° |
| argument of perigee: | 147.5945° |
| revolutions per day: | 14.72336828 |
| mean anomaly at epoch: | 212.6180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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