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 67474U 26145.53215213 +.00000000 +00000-0 +24126-3 0 00009
2 67474 97.4550 219.5560 0013446 186.6045 173.5017 15.23222919 06
| Epoch (UTC): | 25 May 2026 12:46:17 |
| Eccentricity: | 0.0013446 |
| inclination: | 97.4550° |
| perigee height: | 487 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.5560° |
| argument of perigee: | 186.6045° |
| revolutions per day: | 15.23222919 |
| mean anomaly at epoch: | 173.5017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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