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 13080U 26149.19714059 +.00000000 +00000-0 +00000-0 0 00003
2 13080 71.8688 1.8741 5759276 308.3269 12.6146 2.00873467 02
| Epoch (UTC): | 29 May 2026 04:43:52 |
| Eccentricity: | 0.5759276 |
| inclination: | 71.8688° |
| perigee height: | 4874 km |
| apogee height: | 35436 km |
| right ascension of ascending node: | 1.8741° |
| argument of perigee: | 308.3269° |
| revolutions per day: | 2.00873467 |
| mean anomaly at epoch: | 12.6146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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