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 55974U 26145.60214752 +.00000000 +00000-0 +29010-3 0 00003
2 55974 97.5166 317.8534 0004290 156.7675 203.3770 15.47122211 07
| Epoch (UTC): | 25 May 2026 14:27:05 |
| Eccentricity: | 0.0004290 |
| inclination: | 97.5166° |
| perigee height: | 422 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 317.8534° |
| argument of perigee: | 156.7675° |
| revolutions per day: | 15.47122211 |
| mean anomaly at epoch: | 203.3770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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