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 60410U 26145.08914215 +.00000000 +00000-0 +12632-4 0 00000
2 60410 53.1588 69.5359 0001087 84.6139 275.5003 15.69711438 04
| Epoch (UTC): | 25 May 2026 02:08:21 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 69.5359° |
| argument of perigee: | 84.6139° |
| revolutions per day: | 15.69711438 |
| mean anomaly at epoch: | 275.5003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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