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 49761U 26145.33052875 +.00000000 +00000-0 +39673-4 0 00003
2 49761 53.2136 155.0657 0001267 77.0458 283.0676 15.08837736 05
| Epoch (UTC): | 25 May 2026 07:55:57 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.0657° |
| argument of perigee: | 77.0458° |
| revolutions per day: | 15.08837736 |
| mean anomaly at epoch: | 283.0676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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