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 00045U 26133.33518248 +.00000000 +00000-0 +32930-4 0 00002
2 00045 66.6924 92.3811 0249383 186.3382 173.4550 14.35946415 05
| Epoch (UTC): | 13 May 2026 08:02:39 |
| Eccentricity: | 0.0249383 |
| inclination: | 66.6924° |
| perigee height: | 594 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 92.3811° |
| argument of perigee: | 186.3382° |
| revolutions per day: | 14.35946415 |
| mean anomaly at epoch: | 173.4550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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