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 68448U 26145.60746556 +.00000000 +00000-0 +20568-3 0 00004
2 68448 97.4594 104.4721 0004578 132.8099 227.3521 15.18005353 08
| Epoch (UTC): | 25 May 2026 14:34:45 |
| Eccentricity: | 0.0004578 |
| inclination: | 97.4594° |
| perigee height: | 509 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 104.4721° |
| argument of perigee: | 132.8099° |
| revolutions per day: | 15.18005353 |
| mean anomaly at epoch: | 227.3521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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