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 26133.44015508 +.00000000 +00000-0 +74015-4 0 00003
2 29709 98.1348 131.8831 0010941 303.7944 56.2227 14.85916456 05
| Epoch (UTC): | 13 May 2026 10:33:49 |
| Eccentricity: | 0.0010941 |
| inclination: | 98.1348° |
| perigee height: | 603 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 131.8831° |
| argument of perigee: | 303.7944° |
| revolutions per day: | 14.85916456 |
| mean anomaly at epoch: | 56.2227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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