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 67704U 26145.26750625 +.00000000 +00000-0 +82186-3 0 00006
2 67704 97.2822 256.8065 0000964 72.3016 287.8331 15.33456591 00
| Epoch (UTC): | 25 May 2026 06:25:12 |
| Eccentricity: | 0.0000964 |
| inclination: | 97.2822° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.8065° |
| argument of perigee: | 72.3016° |
| revolutions per day: | 15.33456591 |
| mean anomaly at epoch: | 287.8331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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