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 28059U 26067.55830565 +.00000000 +00000-0 +13910-3 0 00002
2 28059 98.6879 62.4187 0047211 234.4331 125.2460 14.55019220 05
| Epoch (UTC): | 08 March 2026 13:23:57 |
| Eccentricity: | 0.0047211 |
| inclination: | 98.6879° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 62.4187° |
| argument of perigee: | 234.4331° |
| revolutions per day: | 14.55019220 |
| mean anomaly at epoch: | 125.2460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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