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 65210U 26145.28507867 +.00000000 +00000-0 +52849-3 0 00009
2 65210 53.1598 156.5176 0000955 99.2488 260.8623 15.34410588 03
| Epoch (UTC): | 25 May 2026 06:50:30 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 156.5176° |
| argument of perigee: | 99.2488° |
| revolutions per day: | 15.34410588 |
| mean anomaly at epoch: | 260.8623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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