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 60335U 26145.50618380 +.00000000 +00000-0 +16635-4 0 00004
2 60335 53.1595 78.9939 0001135 96.4797 263.6333 15.30199612 07
| Epoch (UTC): | 25 May 2026 12:08:54 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.9939° |
| argument of perigee: | 96.4797° |
| revolutions per day: | 15.30199612 |
| mean anomaly at epoch: | 263.6333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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