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 55982U 26145.56971317 +.00000000 +00000-0 +36535-3 0 00004
2 55982 42.0027 333.8376 0006377 198.0618 161.9996 15.38554278 04
| Epoch (UTC): | 25 May 2026 13:40:23 |
| Eccentricity: | 0.0006377 |
| inclination: | 42.0027° |
| perigee height: | 446 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 333.8376° |
| argument of perigee: | 198.0618° |
| revolutions per day: | 15.38554278 |
| mean anomaly at epoch: | 161.9996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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