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 60487U 26145.19372271 +.00000000 +00000-0 +36355-3 0 00003
2 60487 97.3796 228.1994 0001724 31.4798 328.6550 15.38147854 04
| Epoch (UTC): | 25 May 2026 04:38:57 |
| Eccentricity: | 0.0001724 |
| inclination: | 97.3796° |
| perigee height: | 450 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 228.1994° |
| argument of perigee: | 31.4798° |
| revolutions per day: | 15.38147854 |
| mean anomaly at epoch: | 328.6550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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