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 66321U 26145.24803911 +.00000000 +00000-0 +44922-3 0 00001
2 66321 43.0022 140.0781 0001506 272.3995 87.6685 15.27595335 06
| Epoch (UTC): | 25 May 2026 05:57:10 |
| Eccentricity: | 0.0001506 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 140.0781° |
| argument of perigee: | 272.3995° |
| revolutions per day: | 15.27595335 |
| mean anomaly at epoch: | 87.6685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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