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 26041.90116591 +.00000000 +00000-0 +68103-4 0 00005
2 28096 63.6821 353.9507 0074360 120.6250 240.2137 13.41060004 09
| Epoch (UTC): | 10 February 2026 21:37:40 |
| Eccentricity: | 0.0074360 |
| inclination: | 63.6821° |
| perigee height: | 1050 km |
| apogee height: | 1161 km |
| right ascension of ascending node: | 353.9507° |
| argument of perigee: | 120.6250° |
| revolutions per day: | 13.41060004 |
| mean anomaly at epoch: | 240.2137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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