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 60465U 26145.58706791 +.00000000 +00000-0 +25814-3 0 00008
2 60465 34.9913 300.3059 0007332 344.1358 15.9128 15.27360818 02
| Epoch (UTC): | 25 May 2026 14:05:22 |
| Eccentricity: | 0.0007332 |
| inclination: | 34.9913° |
| perigee height: | 479 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 300.3059° |
| argument of perigee: | 344.1358° |
| revolutions per day: | 15.27360818 |
| mean anomaly at epoch: | 15.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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