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 61511U 26145.27227236 +.00000000 +00000-0 +14901-4 0 00005
2 61511 53.1596 146.3066 0001045 71.3701 288.7413 15.31703644 07
| Epoch (UTC): | 25 May 2026 06:32:04 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 146.3066° |
| argument of perigee: | 71.3701° |
| revolutions per day: | 15.31703644 |
| mean anomaly at epoch: | 288.7413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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