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 45016U 26145.63208619 +.00000000 +00000-0 +18544-3 0 00007
2 45016 97.5031 220.0291 0010278 29.0481 331.1319 15.10574005 00
| Epoch (UTC): | 25 May 2026 15:10:12 |
| Eccentricity: | 0.0010278 |
| inclination: | 97.5031° |
| perigee height: | 527 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 220.0291° |
| argument of perigee: | 29.0481° |
| revolutions per day: | 15.10574005 |
| mean anomaly at epoch: | 331.1319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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