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 12889U 26071.66013123 +.00000000 +00000-0 +19570-3 0 00004
2 12889 99.9016 318.2073 1307607 109.2860 279.4942 12.20115631 07
| Epoch (UTC): | 12 March 2026 15:50:35 |
| Eccentricity: | 0.1307607 |
| inclination: | 99.9016° |
| perigee height: | 550 km |
| apogee height: | 2634 km |
| right ascension of ascending node: | 318.2073° |
| argument of perigee: | 109.2860° |
| revolutions per day: | 12.20115631 |
| mean anomaly at epoch: | 279.4942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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