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 54763U 26145.04304126 +.00000000 +00000-0 -16212-4 0 00003
2 54763 53.2151 61.5047 0001690 84.9787 275.1398 15.08846045 02
| Epoch (UTC): | 25 May 2026 01:01:58 |
| Eccentricity: | 0.0001690 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 61.5047° |
| argument of perigee: | 84.9787° |
| revolutions per day: | 15.08846045 |
| mean anomaly at epoch: | 275.1398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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