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 64761U 26145.53893262 +.00000000 +00000-0 +73551-3 0 00007
2 64761 53.1607 245.3753 0000540 21.7236 338.3790 15.34387152 09
| Epoch (UTC): | 25 May 2026 12:56:03 |
| Eccentricity: | 0.0000540 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 245.3753° |
| argument of perigee: | 21.7236° |
| revolutions per day: | 15.34387152 |
| mean anomaly at epoch: | 338.3790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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