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 29709U 26145.62858671 +.00000000 +00000-0 +13227-3 0 00009
2 29709 98.1345 144.3456 0010687 258.9561 101.0452 14.85925975 02
| Epoch (UTC): | 25 May 2026 15:05:09 |
| Eccentricity: | 0.0010687 |
| inclination: | 98.1345° |
| perigee height: | 603 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 144.3456° |
| argument of perigee: | 258.9561° |
| revolutions per day: | 14.85925975 |
| mean anomaly at epoch: | 101.0452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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