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 07735U 26038.61257706 +.00000000 +00000-0 +10132-3 0 00008
2 07735 114.9726 293.9459 0053453 292.5425 67.0005 14.25555624 01
| Epoch (UTC): | 07 February 2026 14:42:06 |
| Eccentricity: | 0.0053453 |
| inclination: | 114.9726° |
| perigee height: | 768 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 293.9459° |
| argument of perigee: | 292.5425° |
| revolutions per day: | 14.25555624 |
| mean anomaly at epoch: | 67.0005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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