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 68034U 26145.40819321 +.00000000 +00000-0 +66534-3 0 00007
2 68034 97.2837 94.4690 0002252 106.2396 253.9094 15.33445778 08
| Epoch (UTC): | 25 May 2026 09:47:47 |
| Eccentricity: | 0.0002252 |
| inclination: | 97.2837° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.4690° |
| argument of perigee: | 106.2396° |
| revolutions per day: | 15.33445778 |
| mean anomaly at epoch: | 253.9094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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