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 64683U 26145.34893620 +.00000000 +00000-0 +53039-3 0 00006
2 64683 53.1599 130.0661 0001131 81.9750 278.1381 15.34404359 02
| Epoch (UTC): | 25 May 2026 08:22:28 |
| Eccentricity: | 0.0001131 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.0661° |
| argument of perigee: | 81.9750° |
| revolutions per day: | 15.34404359 |
| mean anomaly at epoch: | 278.1381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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