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 00059U 26050.17883508 +.00000000 +00000-0 +61161-4 0 00009
2 00059 28.2498 9.8988 0188888 45.1220 316.4498 13.53162066 04
| Epoch (UTC): | 19 February 2026 04:17:31 |
| Eccentricity: | 0.0188888 |
| inclination: | 28.2498° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 9.8988° |
| argument of perigee: | 45.1220° |
| revolutions per day: | 13.53162066 |
| mean anomaly at epoch: | 316.4498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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