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 57519U 26145.63833102 +.00000000 +00000-0 +32365-3 0 00006
2 57519 97.3849 151.2562 0010490 116.3276 243.9039 15.21945427 01
| Epoch (UTC): | 25 May 2026 15:19:11 |
| Eccentricity: | 0.0010490 |
| inclination: | 97.3849° |
| perigee height: | 493 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 151.2562° |
| argument of perigee: | 116.3276° |
| revolutions per day: | 15.21945427 |
| mean anomaly at epoch: | 243.9039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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