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 67052U 26145.54033601 +.00000000 +00000-0 +59526-3 0 00003
2 67052 42.9980 323.9601 0000745 274.4041 85.6725 15.27589546 01
| Epoch (UTC): | 25 May 2026 12:58:05 |
| Eccentricity: | 0.0000745 |
| inclination: | 42.9980° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.9601° |
| argument of perigee: | 274.4041° |
| revolutions per day: | 15.27589546 |
| mean anomaly at epoch: | 85.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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