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 64119U 26145.37507235 +.00000000 +00000-0 +65833-3 0 00002
2 64119 53.1586 27.7021 0001837 77.0403 283.0808 15.42182107 00
| Epoch (UTC): | 25 May 2026 09:00:06 |
| Eccentricity: | 0.0001837 |
| inclination: | 53.1586° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 27.7021° |
| argument of perigee: | 77.0403° |
| revolutions per day: | 15.42182107 |
| mean anomaly at epoch: | 283.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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