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 26052.78229752 +.00000000 +00000-0 +00000-0 0 00005
2 07648 5.7607 284.5181 0012464 284.8983 51.9828 0.99514331 08
| Epoch (UTC): | 21 February 2026 18:46:30 |
| Eccentricity: | 0.0012464 |
| inclination: | 5.7607° |
| perigee height: | 35947 km |
| apogee height: | 36053 km |
| right ascension of ascending node: | 284.5181° |
| argument of perigee: | 284.8983° |
| revolutions per day: | 0.99514331 |
| mean anomaly at epoch: | 51.9828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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