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 06966U 26088.17797505 +.00000000 +00000-0 +12505-3 0 00001
2 06966 74.0568 30.0920 0022027 275.4264 84.4381 14.44838748 05
| Epoch (UTC): | 29 March 2026 04:16:17 |
| Eccentricity: | 0.0022027 |
| inclination: | 74.0568° |
| perigee height: | 727 km |
| apogee height: | 758 km |
| right ascension of ascending node: | 30.0920° |
| argument of perigee: | 275.4264° |
| revolutions per day: | 14.44838748 |
| mean anomaly at epoch: | 84.4381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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