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 44874U 26106.28074997 +.00000000 +00000-0 +49364-4 0 00001
2 44874 98.1518 295.4103 0009354 296.9880 63.0366 14.61921979 01
| Epoch (UTC): | 16 April 2026 06:44:16 |
| Eccentricity: | 0.0009354 |
| inclination: | 98.1518° |
| perigee height: | 680 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 295.4103° |
| argument of perigee: | 296.9880° |
| revolutions per day: | 14.61921979 |
| mean anomaly at epoch: | 63.0366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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