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 67503U 26144.99560184 +.00000000 +00000-0 +51703-3 0 00002
2 67503 42.9989 243.3097 0001499 291.0868 68.9823 15.27585116 06
| Epoch (UTC): | 24 May 2026 23:53:39 |
| Eccentricity: | 0.0001499 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.3097° |
| argument of perigee: | 291.0868° |
| revolutions per day: | 15.27585116 |
| mean anomaly at epoch: | 68.9823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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