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 29713U 26075.80414896 +.00000000 +00000-0 +20880-3 0 00006
2 29713 98.0284 105.5107 0020331 53.1309 307.1772 14.97960596 07
| Epoch (UTC): | 16 March 2026 19:17:58 |
| Eccentricity: | 0.0020331 |
| inclination: | 98.0284° |
| perigee height: | 559 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 105.5107° |
| argument of perigee: | 53.1309° |
| revolutions per day: | 14.97960596 |
| mean anomaly at epoch: | 307.1772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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