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 55637U 26145.29681322 +.00000000 +00000-0 -62811-5 0 00004
2 55637 69.9997 351.4143 0003031 265.7712 94.3100 14.98337280 07
| Epoch (UTC): | 25 May 2026 07:07:24 |
| Eccentricity: | 0.0003031 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.4143° |
| argument of perigee: | 265.7712° |
| revolutions per day: | 14.98337280 |
| mean anomaly at epoch: | 94.3100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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