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 67705U 26145.58562351 +.00000000 +00000-0 +93201-3 0 00009
2 67705 97.2853 257.1356 0001508 93.7600 266.3815 15.33457628 04
| Epoch (UTC): | 25 May 2026 14:03:17 |
| Eccentricity: | 0.0001508 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 257.1356° |
| argument of perigee: | 93.7600° |
| revolutions per day: | 15.33457628 |
| mean anomaly at epoch: | 266.3815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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