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 26069.85335387 +.00000000 +00000-0 +45591-3 0 00002
2 12987 82.4937 349.3259 0010995 164.3115 195.8471 15.33935887 09
| Epoch (UTC): | 10 March 2026 20:28:49 |
| Eccentricity: | 0.0010995 |
| inclination: | 82.4937° |
| perigee height: | 457 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 349.3259° |
| argument of perigee: | 164.3115° |
| revolutions per day: | 15.33935887 |
| mean anomaly at epoch: | 195.8471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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