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 60268U 26145.04625044 +.00000000 +00000-0 +48475-4 0 00000
2 60268 53.1602 57.4544 0001177 74.7137 285.3994 15.30204772 06
| Epoch (UTC): | 25 May 2026 01:06:36 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.4544° |
| argument of perigee: | 74.7137° |
| revolutions per day: | 15.30204772 |
| mean anomaly at epoch: | 285.3994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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