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 67712U 26145.58290618 +.00000000 +00000-0 +61642-3 0 00005
2 67712 97.2852 257.1443 0000766 97.1869 262.9461 15.33449634 05
| Epoch (UTC): | 25 May 2026 13:59:23 |
| Eccentricity: | 0.0000766 |
| inclination: | 97.2852° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1443° |
| argument of perigee: | 97.1869° |
| revolutions per day: | 15.33449634 |
| mean anomaly at epoch: | 262.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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