▸Orbital parameters

Orbit class	GEO
Inclination	0.0390°
Eccentricity	0.0002264
Period	1436.2 min
Apogee	35,798 km
Perigee	35,778 km
Mean motion	1.00266945 rev/day
RAAN	182.9642°
Arg of perigee	274.6834°
Mean anomaly	126.2036°
B*	0.0000e+0
Rev at epoch	772

▸Two-line element set (TLE)

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

1 59915U 24104A 26187.72488556 .00000169 00000-0 00000-0 0 9995

2 59915 0.0390 182.9642 0002264 274.6834 126.2036 1.00266945 7722

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PAKSAT-MM1",
  "OBJECT_ID": "2024-104A",
  "EPOCH": "2026-07-06T17:23:50.112+00:00",
  "MEAN_MOTION": 1.00266945,
  "ECCENTRICITY": 0.0002264,
  "INCLINATION": 0.039,
  "RA_OF_ASC_NODE": 182.9642,
  "ARG_OF_PERICENTER": 274.6834,
  "MEAN_ANOMALY": 126.2036,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 59915,
  "REV_AT_EPOCH": 772,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000169,
  "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	PAKSAT-MM1
Operator	Space and Upper Atmosphere Research CommissionHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Pakistan
Launch date	May 30, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5400HIGHvia 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/59915

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