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 26041.97573458 +.00000000 +00000-0 +67720-4 0 00005
2 28096 63.6822 353.7624 0074355 120.6191 240.2195 13.41060015 02
| Epoch (UTC): | 10 February 2026 23:25:03 |
| Eccentricity: | 0.0074355 |
| inclination: | 63.6822° |
| perigee height: | 1050 km |
| apogee height: | 1161 km |
| right ascension of ascending node: | 353.7624° |
| argument of perigee: | 120.6191° |
| revolutions per day: | 13.41060015 |
| mean anomaly at epoch: | 240.2195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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