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 60460U 26145.60499196 +.00000000 +00000-0 +36619-3 0 00009
2 60460 34.9992 304.5550 0006095 355.4542 4.6116 15.23174812 06
| Epoch (UTC): | 25 May 2026 14:31:11 |
| Eccentricity: | 0.0006095 |
| inclination: | 34.9992° |
| perigee height: | 492 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 304.5550° |
| argument of perigee: | 355.4542° |
| revolutions per day: | 15.23174812 |
| mean anomaly at epoch: | 4.6116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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