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 65661U 26145.12721580 +.00000000 +00000-0 +27076-3 0 00006
2 65661 97.4491 189.0461 0002116 115.3905 244.7542 15.05655201 01
| Epoch (UTC): | 25 May 2026 03:03:11 |
| Eccentricity: | 0.0002116 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.0461° |
| argument of perigee: | 115.3905° |
| revolutions per day: | 15.05655201 |
| mean anomaly at epoch: | 244.7542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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