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 67453U 26145.01693005 +.00000000 +00000-0 +58802-3 0 00006
2 67453 43.0028 134.3148 0002262 266.2441 93.8152 15.27606600 06
| Epoch (UTC): | 25 May 2026 00:24:22 |
| Eccentricity: | 0.0002262 |
| inclination: | 43.0028° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 134.3148° |
| argument of perigee: | 266.2441° |
| revolutions per day: | 15.27606600 |
| mean anomaly at epoch: | 93.8152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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