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 68429U 26144.86143713 +.00000000 +00000-0 +52807-3 0 00007
2 68429 97.4492 103.6725 0005017 101.8143 258.3654 15.18856851 02
| Epoch (UTC): | 24 May 2026 20:40:28 |
| Eccentricity: | 0.0005017 |
| inclination: | 97.4492° |
| perigee height: | 506 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 103.6725° |
| argument of perigee: | 101.8143° |
| revolutions per day: | 15.18856851 |
| mean anomaly at epoch: | 258.3654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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