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 28096U 26074.56221215 +.00000000 +00000-0 +13354-3 0 00000
2 28096 63.6785 271.4996 0073165 116.9744 243.8779 13.41063975 03
| Epoch (UTC): | 15 March 2026 13:29:35 |
| Eccentricity: | 0.0073165 |
| inclination: | 63.6785° |
| perigee height: | 1051 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 271.4996° |
| argument of perigee: | 116.9744° |
| revolutions per day: | 13.41063975 |
| mean anomaly at epoch: | 243.8779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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