▸Orbital parameters

Orbit class	SSO
Inclination	97.9085°
Eccentricity	0.0067109
Period	97.7 min
Apogee	695 km
Perigee	600 km
Mean motion	14.74244511 rev/day
RAAN	320.6105°
Arg of perigee	136.1469°
Mean anomaly	224.5095°
B*	1.0714e-4
Rev at epoch	64,646

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40018U 14033J 26187.89098000 .00000682 00000-0 10714-3 0 9994

2 40018 97.9085 320.6105 0067109 136.1469 224.5095 14.74244511646469

▸ source OMM (JSON)

{
  "OBJECT_NAME": "APRIZESAT 9",
  "OBJECT_ID": "2014-033J",
  "EPOCH": "2026-07-06T21:23:00.672+00:00",
  "MEAN_MOTION": 14.74244511,
  "ECCENTRICITY": 0.0067109,
  "INCLINATION": 97.9085,
  "RA_OF_ASC_NODE": 320.6105,
  "ARG_OF_PERICENTER": 136.1469,
  "MEAN_ANOMALY": 224.5095,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40018,
  "REV_AT_EPOCH": 64646,
  "BSTAR": 0.00010714,
  "MEAN_MOTION_DOT": 0.00000682,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	APRIZESAT 9
Operator	SpaceQuestHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 19, 2014HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	14HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/40018

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.