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 13149U 26088.19781014 +.00000000 +00000-0 +10263-3 0 00001
2 13149 74.0398 131.4551 0014305 269.5566 90.3948 14.36696057 03
| Epoch (UTC): | 29 March 2026 04:44:50 |
| Eccentricity: | 0.0014305 |
| inclination: | 74.0398° |
| perigee height: | 759 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 131.4551° |
| argument of perigee: | 269.5566° |
| revolutions per day: | 14.36696057 |
| mean anomaly at epoch: | 90.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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