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 07648U 26106.74628132 +.00000000 +00000-0 +00000-0 0 00006
2 07648 5.6252 283.9703 0011833 281.4196 308.3928 0.99509282 03
| Epoch (UTC): | 16 April 2026 17:54:38 |
| Eccentricity: | 0.0011833 |
| inclination: | 5.6252° |
| perigee height: | 35952 km |
| apogee height: | 36052 km |
| right ascension of ascending node: | 283.9703° |
| argument of perigee: | 281.4196° |
| revolutions per day: | 0.99509282 |
| mean anomaly at epoch: | 308.3928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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