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 60330U 26145.52201692 +.00000000 +00000-0 -25695-4 0 00002
2 60330 53.1602 79.0945 0000995 96.4673 263.6441 15.30198766 05
| Epoch (UTC): | 25 May 2026 12:31:42 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 79.0945° |
| argument of perigee: | 96.4673° |
| revolutions per day: | 15.30198766 |
| mean anomaly at epoch: | 263.6441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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