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 67013U 26145.38964523 +.00000000 +00000-0 +37656-3 0 00008
2 67013 70.0007 261.1893 0003732 264.3961 95.6772 14.98338006 07
| Epoch (UTC): | 25 May 2026 09:21:05 |
| Eccentricity: | 0.0003732 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 261.1893° |
| argument of perigee: | 264.3961° |
| revolutions per day: | 14.98338006 |
| mean anomaly at epoch: | 95.6772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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