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 61571U 26145.57055880 +.00000000 +00000-0 +49212-4 0 00001
2 61571 97.9097 154.0141 0001698 60.7157 299.4225 14.80936231 09
| Epoch (UTC): | 25 May 2026 13:41:36 |
| Eccentricity: | 0.0001698 |
| inclination: | 97.9097° |
| perigee height: | 625 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 154.0141° |
| argument of perigee: | 60.7157° |
| revolutions per day: | 14.80936231 |
| mean anomaly at epoch: | 299.4225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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