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 65419U 26145.42418123 +.00000000 +00000-0 +35047-3 0 00003
2 65419 53.1593 235.1503 0000736 103.2776 256.8307 15.31716977 02
| Epoch (UTC): | 25 May 2026 10:10:49 |
| Eccentricity: | 0.0000736 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.1503° |
| argument of perigee: | 103.2776° |
| revolutions per day: | 15.31716977 |
| mean anomaly at epoch: | 256.8307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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