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 12994U 26150.45008323 +.00000000 +00000-0 +00000-0 0 00007
2 12994 11.2834 327.2203 0046749 268.6886 266.6567 0.99461937 05
| Epoch (UTC): | 30 May 2026 10:48:07 |
| Eccentricity: | 0.0046749 |
| inclination: | 11.2834° |
| perigee height: | 35817 km |
| apogee height: | 36213 km |
| right ascension of ascending node: | 327.2203° |
| argument of perigee: | 268.6886° |
| revolutions per day: | 0.99461937 |
| mean anomaly at epoch: | 266.6567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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