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 12987U 26073.24541948 +.00000000 +00000-0 +42811-3 0 00004
2 12987 82.4940 345.8775 0011447 153.0241 207.1599 15.34026238 05
| Epoch (UTC): | 14 March 2026 05:53:24 |
| Eccentricity: | 0.0011447 |
| inclination: | 82.4940° |
| perigee height: | 456 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 345.8775° |
| argument of perigee: | 153.0241° |
| revolutions per day: | 15.34026238 |
| mean anomaly at epoch: | 207.1599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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