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 68557U 26145.31126920 +.00000000 +00000-0 +54665-3 0 00005
2 68557 53.1580 6.1236 0000822 77.0507 283.0588 15.34408220 04
| Epoch (UTC): | 25 May 2026 07:28:13 |
| Eccentricity: | 0.0000822 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.1236° |
| argument of perigee: | 77.0507° |
| revolutions per day: | 15.34408220 |
| mean anomaly at epoch: | 283.0588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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