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 60018U 26145.51672183 +.00000000 +00000-0 +18981-3 0 00009
2 60018 53.1582 78.9404 0001660 88.0504 272.0687 15.30198737 07
| Epoch (UTC): | 25 May 2026 12:24:04 |
| Eccentricity: | 0.0001660 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.9404° |
| argument of perigee: | 88.0504° |
| revolutions per day: | 15.30198737 |
| mean anomaly at epoch: | 272.0687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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