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 12759U 26101.29015455 +.00000000 +00000-0 +43761-3 0 00002
2 12759 82.8573 107.0111 0047576 87.7615 289.6690 14.04937823 04
| Epoch (UTC): | 11 April 2026 06:57:49 |
| Eccentricity: | 0.0047576 |
| inclination: | 82.8573° |
| perigee height: | 842 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 107.0111° |
| argument of perigee: | 87.7615° |
| revolutions per day: | 14.04937823 |
| mean anomaly at epoch: | 289.6690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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