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 26104.16822931 +.00000000 +00000-0 +00000-0 0 00003
2 07648 5.6317 283.9966 0011853 281.8144 104.4151 0.99508094 08
| Epoch (UTC): | 14 April 2026 04:02:15 |
| Eccentricity: | 0.0011853 |
| inclination: | 5.6317° |
| perigee height: | 35952 km |
| apogee height: | 36052 km |
| right ascension of ascending node: | 283.9966° |
| argument of perigee: | 281.8144° |
| revolutions per day: | 0.99508094 |
| mean anomaly at epoch: | 104.4151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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