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 67604U 26145.41801207 +.00000000 +00000-0 +36751-3 0 00002
2 67604 97.2850 210.5517 0000306 104.0907 256.0370 15.33451222 08
| Epoch (UTC): | 25 May 2026 10:01:56 |
| Eccentricity: | 0.0000306 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5517° |
| argument of perigee: | 104.0907° |
| revolutions per day: | 15.33451222 |
| mean anomaly at epoch: | 256.0370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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