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 56164U 26088.16756417 +.00000000 +00000-0 +58650-4 0 00004
2 56164 81.0018 148.5737 0005988 177.0975 183.0217 13.84804079 09
| Epoch (UTC): | 29 March 2026 04:01:17 |
| Eccentricity: | 0.0005988 |
| inclination: | 81.0018° |
| perigee height: | 943 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 148.5737° |
| argument of perigee: | 177.0975° |
| revolutions per day: | 13.84804079 |
| mean anomaly at epoch: | 183.0217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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