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 59612U 26145.50870285 +.00000000 +00000-0 +13224-3 0 00004
2 59612 43.0025 320.4003 0001233 272.6703 87.4008 15.27592271 05
| Epoch (UTC): | 25 May 2026 12:12:31 |
| Eccentricity: | 0.0001233 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.4003° |
| argument of perigee: | 272.6703° |
| revolutions per day: | 15.27592271 |
| mean anomaly at epoch: | 87.4008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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