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 68330U 26145.54628105 +.00000000 +00000-0 +54470-3 0 00005
2 68330 53.1590 351.2315 0001400 129.4353 230.6772 15.31049302 02
| Epoch (UTC): | 25 May 2026 13:06:38 |
| Eccentricity: | 0.0001400 |
| inclination: | 53.1590° |
| perigee height: | 472 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 351.2315° |
| argument of perigee: | 129.4353° |
| revolutions per day: | 15.31049302 |
| mean anomaly at epoch: | 230.6772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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