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 67116U 26145.14704007 +.00000000 +00000-0 +61418-3 0 00008
2 67116 42.9974 96.8346 0000398 206.4698 153.6134 15.27589552 01
| Epoch (UTC): | 25 May 2026 03:31:44 |
| Eccentricity: | 0.0000398 |
| inclination: | 42.9974° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 96.8346° |
| argument of perigee: | 206.4698° |
| revolutions per day: | 15.27589552 |
| mean anomaly at epoch: | 153.6134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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