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 60737U 26145.34504653 +.00000000 +00000-0 -75762-7 0 00009
2 60737 53.1616 272.6197 0001329 87.4018 272.7135 15.30203796 07
| Epoch (UTC): | 25 May 2026 08:16:52 |
| Eccentricity: | 0.0001329 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 272.6197° |
| argument of perigee: | 87.4018° |
| revolutions per day: | 15.30203796 |
| mean anomaly at epoch: | 272.7135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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