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 54377U 26145.24740578 +.00000000 +00000-0 +00000-0 0 00004
2 54377 64.7398 193.4732 0011819 223.2416 136.7371 2.13102034 08
| Epoch (UTC): | 25 May 2026 05:56:15 |
| Eccentricity: | 0.0011819 |
| inclination: | 64.7398° |
| perigee height: | 19100 km |
| apogee height: | 19160 km |
| right ascension of ascending node: | 193.4732° |
| argument of perigee: | 223.2416° |
| revolutions per day: | 2.13102034 |
| mean anomaly at epoch: | 136.7371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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