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 67019U 26145.40233284 +.00000000 +00000-0 +35499-3 0 00003
2 67019 70.0008 261.2320 0003518 268.0698 92.0058 14.98339240 09
| Epoch (UTC): | 25 May 2026 09:39:21 |
| Eccentricity: | 0.0003518 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.2320° |
| argument of perigee: | 268.0698° |
| revolutions per day: | 14.98339240 |
| mean anomaly at epoch: | 92.0058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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