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 13000U 26071.20588786 +.00000000 +00000-0 -15313-2 0 00003
2 13000 82.9573 113.3104 0017969 16.2589 48.8246 12.06919647 03
| Epoch (UTC): | 12 March 2026 04:56:28 |
| Eccentricity: | 0.0017969 |
| inclination: | 82.9573° |
| perigee height: | 1636 km |
| apogee height: | 1664 km |
| right ascension of ascending node: | 113.3104° |
| argument of perigee: | 16.2589° |
| revolutions per day: | 12.06919647 |
| mean anomaly at epoch: | 48.8246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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