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 67412U 26145.43334574 +.00000000 +00000-0 +57036-3 0 00008
2 67412 43.0030 164.5630 0001419 266.2069 93.8620 15.27592152 00
| Epoch (UTC): | 25 May 2026 10:24:01 |
| Eccentricity: | 0.0001419 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5630° |
| argument of perigee: | 266.2069° |
| revolutions per day: | 15.27592152 |
| mean anomaly at epoch: | 93.8620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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