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 68270U 26144.78354135 +.00000000 +00000-0 +64382-3 0 00005
2 68270 53.1593 326.3639 0001098 81.1755 278.9372 15.34398846 07
| Epoch (UTC): | 24 May 2026 18:48:17 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 326.3639° |
| argument of perigee: | 81.1755° |
| revolutions per day: | 15.34398846 |
| mean anomaly at epoch: | 278.9372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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