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 67620U 26145.49297122 +.00000000 +00000-0 +61463-3 0 00001
2 67620 43.0022 65.6795 0000553 57.7357 302.3548 15.27589227 02
| Epoch (UTC): | 25 May 2026 11:49:52 |
| Eccentricity: | 0.0000553 |
| inclination: | 43.0022° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 65.6795° |
| argument of perigee: | 57.7357° |
| revolutions per day: | 15.27589227 |
| mean anomaly at epoch: | 302.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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