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 60020U 26145.20069346 +.00000000 +00000-0 +52084-4 0 00002
2 60020 53.1611 80.5273 0001222 90.1768 269.9373 15.30195901 03
| Epoch (UTC): | 25 May 2026 04:48:59 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.5273° |
| argument of perigee: | 90.1768° |
| revolutions per day: | 15.30195901 |
| mean anomaly at epoch: | 269.9373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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