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 26112.26351529 +.00000000 +00000-0 +15634-3 0 00003
2 29499 98.3275 217.2381 0173398 247.4989 193.5474 14.75714191 00
| Epoch (UTC): | 22 April 2026 06:19:27 |
| Eccentricity: | 0.0173398 |
| inclination: | 98.3275° |
| perigee height: | 521 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 217.2381° |
| argument of perigee: | 247.4989° |
| revolutions per day: | 14.75714191 |
| mean anomaly at epoch: | 193.5474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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