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 26032.44724998 +.00000000 +00000-0 +31686-3 0 00003
2 29499 98.3265 135.0343 0176298 141.8468 282.7643 14.75382568 03
| Epoch (UTC): | 01 February 2026 10:44:02 |
| Eccentricity: | 0.0176298 |
| inclination: | 98.3265° |
| perigee height: | 520 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 135.0343° |
| argument of perigee: | 141.8468° |
| revolutions per day: | 14.75382568 |
| mean anomaly at epoch: | 282.7643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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