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 68457U 26145.57870622 +.00000000 +00000-0 +45990-3 0 00008
2 68457 97.4531 104.4232 0003844 81.0196 279.1473 15.18975625 03
| Epoch (UTC): | 25 May 2026 13:53:20 |
| Eccentricity: | 0.0003844 |
| inclination: | 97.4531° |
| perigee height: | 506 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 104.4232° |
| argument of perigee: | 81.0196° |
| revolutions per day: | 15.18975625 |
| mean anomaly at epoch: | 279.1473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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