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 29499U 26144.88141439 +.00000000 +00000-0 +30116-3 0 00005
2 29499 98.3308 250.8574 0175123 143.4116 326.4778 14.75848345 02
| Epoch (UTC): | 24 May 2026 21:09:14 |
| Eccentricity: | 0.0175123 |
| inclination: | 98.3308° |
| perigee height: | 520 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 250.8574° |
| argument of perigee: | 143.4116° |
| revolutions per day: | 14.75848345 |
| mean anomaly at epoch: | 326.4778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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