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 68337U 26145.55596605 +.00000000 +00000-0 +82446-3 0 00006
2 68337 53.1610 346.9873 0001069 101.3716 258.7408 15.35422391 09
| Epoch (UTC): | 25 May 2026 13:20:35 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1610° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 346.9873° |
| argument of perigee: | 101.3716° |
| revolutions per day: | 15.35422391 |
| mean anomaly at epoch: | 258.7408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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