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 67312U 26145.58651786 +.00000000 +00000-0 +98132-3 0 00002
2 67312 42.9989 250.6160 0001362 281.0097 79.0601 15.27589821 02
| Epoch (UTC): | 25 May 2026 14:04:35 |
| Eccentricity: | 0.0001362 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.6160° |
| argument of perigee: | 281.0097° |
| revolutions per day: | 15.27589821 |
| mean anomaly at epoch: | 79.0601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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