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 68444U 26145.38942948 +.00000000 +00000-0 +29560-3 0 00009
2 68444 97.4557 104.2363 0003576 80.4830 279.6808 15.18578408 05
| Epoch (UTC): | 25 May 2026 09:20:46 |
| Eccentricity: | 0.0003576 |
| inclination: | 97.4557° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.2363° |
| argument of perigee: | 80.4830° |
| revolutions per day: | 15.18578408 |
| mean anomaly at epoch: | 279.6808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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