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 24278U 26039.07372587 +.00000000 +00000-0 +13079-4 0 00009
2 24278 98.5420 265.4940 0350817 71.4809 292.4110 13.53266656 08
| Epoch (UTC): | 08 February 2026 01:46:09 |
| Eccentricity: | 0.0350817 |
| inclination: | 98.5420° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 265.4940° |
| argument of perigee: | 71.4809° |
| revolutions per day: | 13.53266656 |
| mean anomaly at epoch: | 292.4110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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