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 68027U 26145.33205904 +.00000000 +00000-0 +68154-3 0 00007
2 68027 97.2854 94.4253 0001192 106.8004 253.3370 15.33452633 07
| Epoch (UTC): | 25 May 2026 07:58:09 |
| Eccentricity: | 0.0001192 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 94.4253° |
| argument of perigee: | 106.8004° |
| revolutions per day: | 15.33452633 |
| mean anomaly at epoch: | 253.3370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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