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 26018.99734536 +.00000000 +00000-0 +11306-3 0 00001
2 00029 48.3795 13.5427 0022598 344.7408 15.2822 14.78502419 08
| Epoch (UTC): | 18 January 2026 23:56:10 |
| Eccentricity: | 0.0022598 |
| inclination: | 48.3795° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 13.5427° |
| argument of perigee: | 344.7408° |
| revolutions per day: | 14.78502419 |
| mean anomaly at epoch: | 15.2822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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