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MERCURY ONE (M1)

In orbit NORAD 66742 YXPN-6198-5145-0440-6603

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
MERCURY ONE (M1)
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-11-28 18:44:30
Separation time
2025-11-28 20:05:36
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.96 km
Apogee
501.90 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6879.6 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66742U 25276CE  26287.15139729  .00004760  00000-0  22123-3 0  9999
2 66742 97.4083 358.6609 0000682 280.3371 79.7787 15.20456091 48498
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 20:55:44 MERCURY ONE (M1)
NORAD 66742
FALCON 9 DEB
NORAD 48610
3.012 12.92 2.9e-07
2026-10-17 22:04:42 TANDEM-X
NORAD 36605
MERCURY ONE (M1)
NORAD 66742
2.723 8.16 5.1e-07
2026-10-17 22:04:42 TERRASAR-X
NORAD 31698
MERCURY ONE (M1)
NORAD 66742
2.959 8.16 4.4e-07
2026-10-18 00:39:19 KANOPUS-V-IK
NORAD 42825
MERCURY ONE (M1)
NORAD 66742
4.672 15.01 7.4e-08
2026-10-18 07:29:46 FLOCK 4H-18
NORAD 66721
MERCURY ONE (M1)
NORAD 66742
4.835 0.01 1.9e-07
2026-10-18 09:57:11 MERCURY ONE (M1)
NORAD 66742
TRANSPORTER-16 OBJECT AT
NORAD 68457
3.675 12.65 2.0e-07
2026-10-18 10:44:33 MERCURY ONE (M1)
NORAD 66742
TRANSPORTER-16 OBJECT AT
NORAD 68457
4.108 12.67 1.6e-07
2026-10-18 20:11:03 ASNARO
NORAD 40298
MERCURY ONE (M1)
NORAD 66742
4.760 0.17 1.9e-07
2026-10-19 05:38:53 IRIDE-MS1-EAGLET 2-4
NORAD 66698
MERCURY ONE (M1)
NORAD 66742
2.095 0.01 1.0e-06
2026-10-19 06:19:50 IRIDE-MS1-EAGLET 2-4
NORAD 66698
MERCURY ONE (M1)
NORAD 66742
3.074 0.01 1.0e-06
2026-10-19 17:29:33 FLOCK 4H-23
NORAD 66726
MERCURY ONE (M1)
NORAD 66742
4.770 0.03 1.9e-07
2026-10-19 20:42:19 OBJECT B
NORAD 62726
MERCURY ONE (M1)
NORAD 66742
4.869 0.02 1.8e-07
2026-10-19 21:25:02 OBJECT B
NORAD 62726
MERCURY ONE (M1)
NORAD 66742
4.338 0.02 2.3e-07
2026-10-19 22:16:50 MERCURY ONE (M1)
NORAD 66742
IRIDE-MS1-EAGLET 2-16
NORAD 68452
4.913 12.67 1.1e-07
2026-10-20 09:26:56 SPACEMOBILE-001
NORAD 61047
MERCURY ONE (M1)
NORAD 66742
4.982 11.06 1.3e-07
2026-10-20 11:38:58 FLOCK 4H-32
NORAD 66735
MERCURY ONE (M1)
NORAD 66742
4.685 0.02 2.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite