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 61671U 26145.27553735 +.00000000 +00000-0 -66412-6 0 00005
2 61671 53.1604 95.1754 0001403 85.6898 274.4264 15.30193360 05
| Epoch (UTC): | 25 May 2026 06:36:46 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1754° |
| argument of perigee: | 85.6898° |
| revolutions per day: | 15.30193360 |
| mean anomaly at epoch: | 274.4264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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