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 66898U 26145.39333813 +.00000000 +00000-0 +50027-3 0 00008
2 66898 53.1611 27.4731 0001195 95.4179 264.6960 15.34413480 07
| Epoch (UTC): | 25 May 2026 09:26:24 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.1611° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 27.4731° |
| argument of perigee: | 95.4179° |
| revolutions per day: | 15.34413480 |
| mean anomaly at epoch: | 264.6960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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