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 26106.71990412 +.00000000 +00000-0 +51329-4 0 00003
2 13149 74.0391 97.4212 0014057 234.0201 125.9650 14.36705188 09
| Epoch (UTC): | 16 April 2026 17:16:39 |
| Eccentricity: | 0.0014057 |
| inclination: | 74.0391° |
| perigee height: | 759 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.4212° |
| argument of perigee: | 234.0201° |
| revolutions per day: | 14.36705188 |
| mean anomaly at epoch: | 125.9650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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