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 00029U 26104.00844439 +.00000000 +00000-0 +60679-4 0 00001
2 00029 48.3794 329.6361 0022249 351.2402 8.8120 14.78695733 06
| Epoch (UTC): | 14 April 2026 00:12:09 |
| Eccentricity: | 0.0022249 |
| inclination: | 48.3794° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 329.6361° |
| argument of perigee: | 351.2402° |
| revolutions per day: | 14.78695733 |
| mean anomaly at epoch: | 8.8120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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