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 61754U 26145.64328722 +.00000000 +00000-0 +62054-3 0 00008
2 61754 97.2966 22.1244 0005540 23.2530 336.8975 15.57370520 04
| Epoch (UTC): | 25 May 2026 15:26:20 |
| Eccentricity: | 0.0005540 |
| inclination: | 97.2966° |
| perigee height: | 392 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 22.1244° |
| argument of perigee: | 23.2530° |
| revolutions per day: | 15.57370520 |
| mean anomaly at epoch: | 336.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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