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 65532U 26145.44467687 +.00000000 +00000-0 +26247-3 0 00002
2 65532 97.4467 215.1340 0002519 133.7257 226.4179 15.05653542 08
| Epoch (UTC): | 25 May 2026 10:40:20 |
| Eccentricity: | 0.0002519 |
| inclination: | 97.4467° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1340° |
| argument of perigee: | 133.7257° |
| revolutions per day: | 15.05653542 |
| mean anomaly at epoch: | 226.4179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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