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 60202U 26145.53997384 +.00000000 +00000-0 +61746-4 0 00007
2 60202 53.1607 325.4025 0001005 95.7077 264.4039 15.31700782 08
| Epoch (UTC): | 25 May 2026 12:57:33 |
| Eccentricity: | 0.0001005 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 325.4025° |
| argument of perigee: | 95.7077° |
| revolutions per day: | 15.31700782 |
| mean anomaly at epoch: | 264.4039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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