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 26161.59409663 +.00000000 +00000-0 +18494-3 0 00003
2 29507 97.5460 206.2214 0031228 306.8492 52.9878 15.17735555 04
| Epoch (UTC): | 10 June 2026 14:15:29 |
| Eccentricity: | 0.0031228 |
| inclination: | 97.5460° |
| perigee height: | 491 km |
| apogee height: | 534 km |
| right ascension of ascending node: | 206.2214° |
| argument of perigee: | 306.8492° |
| revolutions per day: | 15.17735555 |
| mean anomaly at epoch: | 52.9878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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