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 67273U 26145.61934251 +.00000000 +00000-0 +13744-3 0 00009
2 67273 97.3962 220.4479 0016014 90.8660 269.4410 15.20981178 00
| Epoch (UTC): | 25 May 2026 14:51:51 |
| Eccentricity: | 0.0016014 |
| inclination: | 97.3962° |
| perigee height: | 492 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 220.4479° |
| argument of perigee: | 90.8660° |
| revolutions per day: | 15.20981178 |
| mean anomaly at epoch: | 269.4410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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