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 64357U 26145.57270992 +.00000000 +00000-0 +18436-3 0 00002
2 64357 70.0003 200.7856 0003506 269.5247 90.5511 14.98335332 06
| Epoch (UTC): | 25 May 2026 13:44:42 |
| Eccentricity: | 0.0003506 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 200.7856° |
| argument of perigee: | 269.5247° |
| revolutions per day: | 14.98335332 |
| mean anomaly at epoch: | 90.5511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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