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 60235U 26040.25328292 +.00000000 +00000-0 +24200-3 0 00005
2 60235 61.9954 316.0273 0062425 106.2615 254.5355 15.00442672 04
| Epoch (UTC): | 09 February 2026 06:04:43 |
| Eccentricity: | 0.0062425 |
| inclination: | 61.9954° |
| perigee height: | 522 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 316.0273° |
| argument of perigee: | 106.2615° |
| revolutions per day: | 15.00442672 |
| mean anomaly at epoch: | 254.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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