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 52641U 26145.38671188 +.00000000 +00000-0 -13508-4 0 00003
2 52641 53.2151 275.0160 0001013 101.1743 258.9363 15.08833095 08
| Epoch (UTC): | 25 May 2026 09:16:51 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 275.0160° |
| argument of perigee: | 101.1743° |
| revolutions per day: | 15.08833095 |
| mean anomaly at epoch: | 258.9363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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