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 67266U 26145.45033421 +.00000000 +00000-0 +38558-3 0 00002
2 67266 97.3963 220.5352 0016038 85.4633 274.8436 15.22974808 02
| Epoch (UTC): | 25 May 2026 10:48:28 |
| Eccentricity: | 0.0016038 |
| inclination: | 97.3963° |
| perigee height: | 486 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 220.5352° |
| argument of perigee: | 85.4633° |
| revolutions per day: | 15.22974808 |
| mean anomaly at epoch: | 274.8436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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