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 12999U 26065.45314792 +.00000000 +00000-0 -12240-2 0 00009
2 12999 82.9617 141.3103 0015181 162.3804 213.4060 12.05305470 01
| Epoch (UTC): | 06 March 2026 10:52:31 |
| Eccentricity: | 0.0015181 |
| inclination: | 82.9617° |
| perigee height: | 1645 km |
| apogee height: | 1669 km |
| right ascension of ascending node: | 141.3103° |
| argument of perigee: | 162.3804° |
| revolutions per day: | 12.05305470 |
| mean anomaly at epoch: | 213.4060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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