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 52671U 26145.48188130 +.00000000 +00000-0 +65911-4 0 00001
2 52671 53.2118 169.3857 0000997 85.7174 274.3932 15.08840047 06
| Epoch (UTC): | 25 May 2026 11:33:54 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.3857° |
| argument of perigee: | 85.7174° |
| revolutions per day: | 15.08840047 |
| mean anomaly at epoch: | 274.3932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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