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 12544U 26150.78448123 +.00000000 +00000-0 +00000-0 0 00000
2 12544 10.3013 319.4829 0029170 17.8971 174.2911 0.98726727 07
| Epoch (UTC): | 30 May 2026 18:49:39 |
| Eccentricity: | 0.0029170 |
| inclination: | 10.3013° |
| perigee height: | 36101 km |
| apogee height: | 36350 km |
| right ascension of ascending node: | 319.4829° |
| argument of perigee: | 17.8971° |
| revolutions per day: | 0.98726727 |
| mean anomaly at epoch: | 174.2911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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