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 04499U 26087.50959773 +.00000000 +00000-0 +13917-3 0 00001
2 04499 101.3549 102.4696 0028556 153.2128 1.4097 12.51297309 07
| Epoch (UTC): | 28 March 2026 12:13:49 |
| Eccentricity: | 0.0028556 |
| inclination: | 101.3549° |
| perigee height: | 1437 km |
| apogee height: | 1481 km |
| right ascension of ascending node: | 102.4696° |
| argument of perigee: | 153.2128° |
| revolutions per day: | 12.51297309 |
| mean anomaly at epoch: | 1.4097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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