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 67262U 26145.16600794 +.00000000 +00000-0 +46271-3 0 00000
2 67262 97.3941 220.2541 0015856 87.3652 272.9400 15.23407161 04
| Epoch (UTC): | 25 May 2026 03:59:03 |
| Eccentricity: | 0.0015856 |
| inclination: | 97.3941° |
| perigee height: | 485 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.2541° |
| argument of perigee: | 87.3652° |
| revolutions per day: | 15.23407161 |
| mean anomaly at epoch: | 272.9400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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