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 64548U 26145.55514123 +.00000000 +00000-0 +25361-3 0 00004
2 64548 97.4747 261.0985 0001847 134.7875 225.3511 15.20819272 09
| Epoch (UTC): | 25 May 2026 13:19:24 |
| Eccentricity: | 0.0001847 |
| inclination: | 97.4747° |
| perigee height: | 502 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 261.0985° |
| argument of perigee: | 134.7875° |
| revolutions per day: | 15.20819272 |
| mean anomaly at epoch: | 225.3511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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