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 68035U 26145.33749760 +.00000000 +00000-0 +63329-3 0 00008
2 68035 97.2841 94.4186 0001421 71.2046 288.9350 15.33460344 03
| Epoch (UTC): | 25 May 2026 08:05:59 |
| Eccentricity: | 0.0001421 |
| inclination: | 97.2841° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 94.4186° |
| argument of perigee: | 71.2046° |
| revolutions per day: | 15.33460344 |
| mean anomaly at epoch: | 288.9350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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