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 67538U 26145.41311134 +.00000000 +00000-0 -15119-3 0 00009
2 67538 97.2860 32.4855 0002089 93.4615 266.6867 15.33427991 02
| Epoch (UTC): | 25 May 2026 09:54:52 |
| Eccentricity: | 0.0002089 |
| inclination: | 97.2860° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4855° |
| argument of perigee: | 93.4615° |
| revolutions per day: | 15.33427991 |
| mean anomaly at epoch: | 266.6867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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