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 65554U 26145.28292808 +.00000000 +00000-0 +18131-3 0 00002
2 65554 49.9801 145.3940 0011008 193.2117 166.8534 14.84088850 07
| Epoch (UTC): | 25 May 2026 06:47:24 |
| Eccentricity: | 0.0011008 |
| inclination: | 49.9801° |
| perigee height: | 609 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 145.3940° |
| argument of perigee: | 193.2117° |
| revolutions per day: | 14.84088850 |
| mean anomaly at epoch: | 166.8534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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