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 68028U 26145.39311919 +.00000000 +00000-0 +42744-3 0 00005
2 68028 97.2840 93.4231 0001848 99.1576 260.9876 15.33443135 06
| Epoch (UTC): | 25 May 2026 09:26:05 |
| Eccentricity: | 0.0001848 |
| inclination: | 97.2840° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 93.4231° |
| argument of perigee: | 99.1576° |
| revolutions per day: | 15.33443135 |
| mean anomaly at epoch: | 260.9876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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