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 26074.48478006 +.00000000 +00000-0 +32107-3 0 00002
2 12987 82.4942 344.6180 0011575 149.1234 211.0691 15.34053789 02
| Epoch (UTC): | 15 March 2026 11:38:04 |
| Eccentricity: | 0.0011575 |
| inclination: | 82.4942° |
| perigee height: | 456 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 344.6180° |
| argument of perigee: | 149.1234° |
| revolutions per day: | 15.34053789 |
| mean anomaly at epoch: | 211.0691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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