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 29507U 26140.09976455 +.00000000 +00000-0 +14034-3 0 00009
2 29507 97.5471 184.7958 0033257 22.8421 337.4283 15.17541567 01
| Epoch (UTC): | 20 May 2026 02:23:39 |
| Eccentricity: | 0.0033257 |
| inclination: | 97.5471° |
| perigee height: | 490 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 184.7958° |
| argument of perigee: | 22.8421° |
| revolutions per day: | 15.17541567 |
| mean anomaly at epoch: | 337.4283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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