▸Orbital parameters

Orbit class	LEO
Inclination	89.9978°
Eccentricity	0.0069239
Period	108.0 min
Apogee	1,185 km
Perigee	1,081 km
Mean motion	13.33595127 rev/day
RAAN	212.5949°
Arg of perigee	192.6035°
Mean anomaly	293.6182°
B*	4.4477e-5
Rev at epoch	96,263

▸Two-line element set (TLE)

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

1 01512U 65065E 26187.58323572 .00000031 00000-0 44477-4 0 9994

2 01512 89.9978 212.5949 0069239 192.6035 293.6182 13.33595127962634

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TEMPSAT 1",
  "OBJECT_ID": "1965-065E",
  "EPOCH": "2026-07-06T13:59:51.566+00:00",
  "MEAN_MOTION": 13.33595127,
  "ECCENTRICITY": 0.0069239,
  "INCLINATION": 89.9978,
  "RA_OF_ASC_NODE": 212.5949,
  "ARG_OF_PERICENTER": 192.6035,
  "MEAN_ANOMALY": 293.6182,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 1512,
  "REV_AT_EPOCH": 96263,
  "BSTAR": 0.000044477,
  "MEAN_MOTION_DOT": 3.1e-7,
  "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	TEMPSAT 1
Operator	Naval Research LabHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 13, 1965HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	9HIGHvia 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/1512

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