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 26075.23332830 +.00000000 +00000-0 +13824-3 0 00003
2 28096 63.6783 269.8050 0073150 116.9088 243.9437 13.41064105 06
| Epoch (UTC): | 16 March 2026 05:35:59 |
| Eccentricity: | 0.0073150 |
| inclination: | 63.6783° |
| perigee height: | 1051 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 269.8050° |
| argument of perigee: | 116.9088° |
| revolutions per day: | 13.41064105 |
| mean anomaly at epoch: | 243.9437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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