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 52897U 26145.57050308 +.00000000 +00000-0 +14593-3 0 00005
2 52897 98.2198 289.5462 0009920 95.4662 264.7672 14.63260279 02
| Epoch (UTC): | 25 May 2026 13:41:31 |
| Eccentricity: | 0.0009920 |
| inclination: | 98.2198° |
| perigee height: | 676 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 289.5462° |
| argument of perigee: | 95.4662° |
| revolutions per day: | 14.63260279 |
| mean anomaly at epoch: | 264.7672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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