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 67134U 26145.54955875 +.00000000 +00000-0 +31632-3 0 00008
2 67134 51.9027 86.9521 0001146 137.7730 222.3319 14.76498408 01
| Epoch (UTC): | 25 May 2026 13:11:21 |
| Eccentricity: | 0.0001146 |
| inclination: | 51.9027° |
| perigee height: | 640 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 86.9521° |
| argument of perigee: | 137.7730° |
| revolutions per day: | 14.76498408 |
| mean anomaly at epoch: | 222.3319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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