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 60030U 26145.52144241 +.00000000 +00000-0 +11818-4 0 00006
2 60030 53.1606 77.5585 0001216 96.2762 263.8379 15.34385534 00
| Epoch (UTC): | 25 May 2026 12:30:52 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 77.5585° |
| argument of perigee: | 96.2762° |
| revolutions per day: | 15.34385534 |
| mean anomaly at epoch: | 263.8379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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