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 01291U 26153.69878528 +.00000000 +00000-0 +53451-4 0 00008
2 01291 70.0798 267.0649 0019531 146.0177 214.2184 13.94973924 08
| Epoch (UTC): | 02 June 2026 16:46:15 |
| Eccentricity: | 0.0019531 |
| inclination: | 70.0798° |
| perigee height: | 897 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 267.0649° |
| argument of perigee: | 146.0177° |
| revolutions per day: | 13.94973924 |
| mean anomaly at epoch: | 214.2184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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