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 64603U 26145.49590812 +.00000000 +00000-0 +46647-3 0 00008
2 64603 53.1595 338.5216 0001480 91.7624 268.3547 15.30211721 07
| Epoch (UTC): | 25 May 2026 11:54:06 |
| Eccentricity: | 0.0001480 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5216° |
| argument of perigee: | 91.7624° |
| revolutions per day: | 15.30211721 |
| mean anomaly at epoch: | 268.3547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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