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 61763U 26145.60886758 +.00000000 +00000-0 +57094-3 0 00000
2 61763 97.3012 21.5188 0005249 32.7702 327.3875 15.50966220 04
| Epoch (UTC): | 25 May 2026 14:36:46 |
| Eccentricity: | 0.0005249 |
| inclination: | 97.3012° |
| perigee height: | 410 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 21.5188° |
| argument of perigee: | 32.7702° |
| revolutions per day: | 15.50966220 |
| mean anomaly at epoch: | 327.3875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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