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 67541U 26145.25812315 +.00000000 +00000-0 +84496-3 0 00005
2 67541 97.2865 32.3918 0001915 96.7915 263.3546 15.33455383 00
| Epoch (UTC): | 25 May 2026 06:11:41 |
| Eccentricity: | 0.0001915 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.3918° |
| argument of perigee: | 96.7915° |
| revolutions per day: | 15.33455383 |
| mean anomaly at epoch: | 263.3546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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